BS EN 4632 005 2009 ICS 49 025 01 NO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAW BRITISH STANDARD Aerospace series — Weldability and brazeability of materials in aerospace cons[.]
BRITISH STANDARD BS EN 4632-005:2009 Part 005: Homogeneous assemblies of heat resisting Ni or Co base alloys ICS 49.025.01 NO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAW Copyright British Standards Institution Provided by IHS under license with BSI - Uncontrolled Copy No reproduction or networking permitted without license from IHS Not for Resale `,,```,,,,````-`-`,,`,,`,`,,` - Aerospace series — Weldability and brazeability of materials in aerospace constructions BS EN 4632-005:2009 National foreword This British Standard is the UK implementation of EN 4632-005:2009 The UK participation in its preparation was entrusted to Technical Committee ACE/61/-/2, Heat Treatment of Metallic Materials for Aerospace Purposes A list of organizations represented on this committee can be obtained on request to its secretary This publication does not purport to include all the necessary provisions of a contract Users are responsible for its correct application Compliance with a British Standard cannot confer immunity from legal obligations Amendments/corrigenda issued since publication Date Comments `,,```,,,,````-`-`,,`,,`,`,,` - This British Standard was published under the authority of the Standards Policy and Strategy Committee on 31 March 2010 © BSI 2010 ISBN 978 580 58876 Copyright British Standards Institution Provided by IHS under license with BSI - Uncontrolled Copy No reproduction or networking permitted without license from IHS Not for Resale BS EN 4632-005:2009 EN 4632-005 EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM December 2009 ICS 49.025.01 English Version Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 005: Homogeneous assemblies of heat resisting Ni or Co base alloys Luft- und Raumfahrt - Schweißbarkeit und Lưtbarkeit von Werkstoffen im Luft und Raumfahrzeugbau- - Teil 005: Schweißen und Lưten gleichartiger Verbindungen aus hitzebeständigen Nickel- oder Kobaltbasislegierungen Série aérospatiale - Assemblages soudés et brasés pour constructions aérospatiales - Soudabilité et brasabilité des matériaux - Partie 005: assemblage homogènes des alliages base Ni ou Co résistant haute température This European Standard was approved by CEN on 12 September 2009 CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this European Standard the status of a national standard without any alteration Up-to-date lists and bibliographical references concerning such national standards may be obtained on application to the CEN Management Centre or to any CEN member This European Standard exists in three official versions (English, French, German) A version in any other language made by translation under the responsibility of a CEN member into its own language and notified to the CEN Management Centre has the same status as the official versions CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom EUROPEAN COMMITTEE FOR STANDARDIZATION COMITÉ EUROPÉEN DE NORMALISATION EUROPÄISCHES KOMITEE FÜR NORMUNG Management Centre: Avenue Marnix 17, B-1000 Brussels © 2009 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members `,,```,,,,````-`-`, Copyright British Standards Institution Provided by IHS under license with BSI - Uncontrolled Copy No reproduction or networking permitted without license from IHS Not for Resale Ref No EN 4632-005:2009: E BS EN 4632-005:2009 EN 4632-005:2009 (E) Contents Page Foreword 3 1 Scope 4 2 Normative references 4 3 Terms, definitions, symbols and abbreviations 7 4 Use of this standard 8 5 Updating this standard 8 6 List of heat resisting Ni or Co base alloys 8 7 Heat resisting Ni or Co base alloys 9 `,,```,,,,````-`-`,,`,,`,`,,` - Copyright British Standards Institution Provided by IHS under license with BSI - Uncontrolled Copy No reproduction or networking permitted without license from IHS Not for Resale BS EN 4632-005:2009 EN 4632-005:2009 (E) Foreword This document (EN 4632-005:2009) has been prepared by the Aerospace and Defence Industries Association of Europe - Standardization (ASD-STAN) After enquiries and votes carried out in accordance with the rules of this Association, this Standard has received the approval of the National Associations and the Official Services of the member countries of ASD, prior to its presentation to CEN This European Standard shall be given the status of a national standard, either by publication of an identical text or by endorsement, at the latest by June 2010, and conflicting national standards shall be withdrawn at the latest by June 2010 Attention is drawn to the possibility that some of the elements of this document may be the subject of patent rights CEN [and/or CENELEC] shall not be held responsible for identifying any or all such patent rights According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following countries are bound to implement this European Standard: Austria, Belgium, Bulgaria, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom `,,```,,,,````-`-`,,`,,`,`,,` - Copyright British Standards Institution Provided by IHS under license with BSI - Uncontrolled Copy No reproduction or networking permitted without license from IHS Not for Resale BS EN 4632-005:2009 EN 4632-005:2009 (E) Scope This European Standard defines degrees of weldability and brazeability for materials or families of materials used in the aerospace industry indicate the main titles, the chemical composition and the main characteristics; contain recommendations for welding and brazing; indicate a degree of weldability or brazeability for a given process under defined conditions; indicate a value of the mechanical strength coefficient of the welded joint for each welding process, when it could be extracted from bibliographic references referring to it The joint coefficient is expressed as a ratio of the tensile strength of the welded joint to the tensile strength of the base alloy (to be in accordance with EN 4632-002) It is applicable without restriction for the manufacturing of new parts or for repair Normative references The following referenced documents are indispensable for the application of this document For dated references, only the edition cited applies For undated references, the latest edition of the referenced document (including any amendments) applies EN 2161, Aerospace series — Heat resisting alloy CO-CH1401 (CoCr26Ni11W) — Not heat treated — Precision castings 1) EN 2183, Aerospace series — Heat resisting alloy NI-PH2301 (NiCr21Fe18Mo9) — Solution treated — Forging — De ≤ 200 mm 1) EN 2184, Aerospace series — Heat resisting alloy NI-PH2301 (NiCr21Fe18Mo9) — Solution treated — Bar and section — De ≤ 200 mm 1) EN 2185, Aerospace series — Heat resisting alloy NI-PH2301 (NiCr21Fe18Mo9) — Solution treated — Sheet, strip and plate — 0,2 mm ≤ a ≤ 10 mm 1) EN 2199, Aerospace series — Heat resisting alloy NI-PH1303 (NiCo20Cr20Mo5Ti2Al) — Solution treated and precipitation treated — Bar and section — De ≤ 200 mm 1) EN 2203, Aerospace series — Heat resisting alloy NI-PH1303 (NiCo20Cr20Mo5Ti2Al) — Solution treated — Sheet, strip and plate — 0,2 mm ≤ a ≤ 10 mm 1) EN 2204, Aerospace series — Heat resisting alloy NI-CH1303 (NiCo20Cr20Mo5Ti2Al) — Vacuum melted — Solution treated and precipitation treated — Precision casting — De ≤ 50 mm 1) EN 2403, Aerospace series — Heat resisting alloy NI-CH2601 (NiCr19Fe19Nb5Mo3) — Vacuum melted — Solution treated and precipitation treated — Precision casting — a or D ≤ 50 mm 1) EN 2405, Aerospace series — Heat resisting alloy NI-PH2601 (NiCr19Fe19Nb5Mo3) — Solution treated and precipitation treated — Forgings — De ≤ 200 mm 1) 1) Published as ASD-STAN Prestandard at the date of publication of this standard Copyright British Standards Institution Provided by IHS under license with BSI - Uncontrolled Copy No reproduction or networking permitted without license from IHS Not for Resale `,,```,,,,````-`-`,,`,,`,`,,` - It comprises a series of sheets, by materials or by material family, which: BS EN 4632-005:2009 EN 4632-005:2009 (E) EN 2407, Aerospace series — Heat resisting alloy NI-PH2601 (NiCr19Fe19Nb5Mo3) — Solution treated and precipitation treated — Sheet, strip and plate — 0,2 mm ≤ a ≤ 10 mm 2) EN 2657, Aerospace series — Heat resisting alloy CO-PH1402 — Consumable electrode remelted — Solution treated — Bar — a or D ≤ 150 mm — Rm ≥ 860 MPa 2) EN 2658, Aerospace series — Heat resisting alloy CO-PH1402 — Consumable electrode remelted — As forged — Forging stock — De ≤ 360 mm 2) EN 2659, Aerospace series — Heat resisting alloy CO-PH1402 — Consumable electrode remelted — Solution treated — Forgings — De ≤ 100 mm — Rm ≥ 860 MPa 2) EN 2661, Aerospace series — Heat resisting alloy CO-PH1402 — Consumable electrode remelted — Solution treated — Sheet and strip — a ≤ mm — Rm ≥ 860 MPa 2) EN 2662, Aerospace series — Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) — Annealed — Sheet, strip and plate — 0,2 mm ≤ a ≤ 10 mm 2) EN 2663, Aerospace series — Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) — Solution treated — Sheet, strip and plate — 0,2 mm ≤ a ≤ 10 mm 2) EN 2959, Aerospace series — Heat resisting alloy NI-PH1302 (NiCr20Co13Mo4Ti3Al) — Solution treated and cold worked — Bar for forged fasteners — mm ≤ D ≤ 30 mm 2) EN 3668, Aerospace series — Heat resisting alloy NI-PH2301 (NiCr21Fe18Mo9) — Non heat treated — Forging stock — a or D ≤ 250 mm EN 3671, Aerospace series — Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) — Non heat treated — Forging stock — a or D ≤ 250 mm EN 3884, Aerospace series — Heat resisting alloy NI-WH2601 (NiCr19Nb5Mo3Ti) — Filler metal for welding EN 3887, Aerospace series — Heat resisting alloy CO-WH4101 (CoCr20W15Ni) — Filler metal for welding EN 3888, Aerospace series — Heat resisting alloy CO-WH1402 (CoCr22Ni22W15) — Filler metal for welding EN 4095, Aerospace series — Heat resisting alloy NI-CH1305 (NiCr16Co10Mo8Al4Ti4) — Vacuum melted — Non heat treated — Precision castings 2) EN 4222, Aerospace series — Heat resisting alloy NI-PH1305 (NiCr22Co13Mo9Al1) — Air melted and vacuum refined — Annealed — Sheet and strip — 0,25 mm ≤ a ≤ mm 2) EN 4327, Aerospace series — Heat resisting alloy CO-WH1401 (CoCr26Ni11W8) — Filler metal for welding — Wire and rod EN 4329, Aerospace series — Heat resisting alloy NI-WH0001 (NiCr20) — Filler metal for welding — Wire and rod EN 4376, Aerospace series — Heat resisting alloy NI-PH2601 (NiCr19Fe19Nb5Mo3) — Solution treated and precipitation treated — Bar and section — De ≤ 200 mm 2) EN 4377, Aerospace series — Heat resisting alloy NI-PH2601 (NiCr19Fe19Nb5Mo3) — Non heat treated — Forging stock — a or D ≤ 300 mm 2) 2) Published as ASD-STAN Prestandard at the date of publication of this standard `,,```,,,,````-`-`,,`,,`,`,,` - Copyright British Standards Institution Provided by IHS under license with BSI - Uncontrolled Copy No reproduction or networking permitted without license from IHS Not for Resale BS EN 4632-005:2009 EN 4632-005:2009 (E) EN 4379, Aerospace series — Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) — Solution treated — Forging — De ≤ 200 mm EN 4380, Aerospace series — Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) — Solution treated — Bar and section — De ≤ 200 mm 3) EN 4381, Aerospace series — Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) — Solution treated — Seamless tubes — For structural application — D ≤ 50 mm, a ≤ mm 3) EN 4384, Aerospace series — Heat resisting alloy NI-CH1303 (NiCo20Cr20Mo5Ti2Al) — Non heat treated — Remelting stock EN 4566, Aerospace series — Heat resisting alloy CO-PH4101 (CoCr20W15Ni) — Vacuum melted — Solution treated — Forgings — De ≤ 100 mm 3) EN 4567, Aerospace series — Heat resisting alloy CO-PH4101 (CoCr20W15Ni) — Vacuum melted — Solution treated — Bar and section — a or D ≤ 100 mm 3) EN 4568, Aerospace series — Heat resisting alloy CO-PH4101 (CoCr20W15Ni) — Vacuum melted — Solution treated — Sheet and strip — a ≤ mm 3) EN 4569, Aerospace series — Heat resisting alloy CO-PH4101 (CoCr20W15Ni) — Vacuum melted — Solution treated — Wire — D ≤ mm 3) EN 4632-001:2008, Aerospace series — Welded and brazed assemblies for aerospace constructions — Weldability and brazeability of materials — Part 001: General requirements EN 4632-002, Aerospace series — Welded and brazed assemblies for aerospace constructions — Weldability and brazeability of materials — Part 002: Homogeneous asssemblies aluminium and aluminium alloys EN 10095, Heat resisting steels and nickel alloys EN ISO 4063:2009, Welding and allied processes — Nomenclature of processes and reference numbers (ISO 4063:2009) EN ISO 18274, Welding consumables — Wire and strips electrodes, wires and rods for fusion welding of nickel and nickel alloys — Classification (ISO 18274:2004) ISO 9722, Nickel and nickel alloys — Composition and forms of wrought products AMS 5390, Nickel alloy, corrosion and heat resistant, investment castings 47.5Ni - 22Cr - 1.5Co - 9Mo 0.60W - 18.5Fe (N-12mv) as cast 4) AMS 5399, Nickel alloy, corrosion and heat resistant, investment castings 52Ni - 19Cr - 11Co - 9.8Mo - 3.2Ti 1.6Al - 0.006B vacuum-melted, vacuum-cast, solution heat treated 4) AMS 5402, Nickel alloy, corrosion and heat-resistant, investment castings 62Ni - 21.5Cr - 9.0Mo - 3.6Cb (Nb) as cast 4) 3) Published as ASD-STAN Prestandard at the date of publication of this standard 4) Published by: SAE, 400 Commonwealth Drive - Warrendale, PA 15096-0001 USA Copyright British Standards Institution Provided by IHS under license with BSI - Uncontrolled Copy No reproduction or networking permitted without license from IHS Not for Resale `,,```,,,,````-`-`,,`,,`,`,,` - EN 4382, Aerospace series — Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) — Solution treated — Seamless tubes — For hydraulic application — D ≤ 50 mm, a ≤ mm BS EN 4632-005:2009 EN 4632-005:2009 (E) AMS 5540, Nickel alloy, corrosion and heat resistant, sheet, strip, and plate 74Ni - 15.5Cr - 8.0Fe annealed 5) AMS 5580, Nickel alloy, corrosion and heat resistant, seamless tubing 74Ni - 15.5Cr - 8.0Fe annealed 5) AMS 5665, Nickel alloy, corrosion and heat resistant, bars, forgings, and rings 74Ni - 15.5Cr - 8.0Fe 5) AMS 5687, Nickel alloy, corrosion and heat resistant, wire 74Ni - 15.5Cr - 8.0Fe annealed 5) AWS A5.14, Specification for Nickel and Nickel Alloy Bare Welding Electrodes and Rods 6) AWS A5.8-92, Specification for filler metals for brazing and braze welding 6) Terms, definitions, symbols and abbreviations For the purposes of this document, the terms and definitions given in EN 4632-001:2008 and EN ISO 4063:2009 apply `,,```,,,,````-`-`,,`,,`,`,,` - F : Foil p : Powder PJHT : Post joining heat treatment PWHT : Post-weld heat treatment w : Wire 15 : Plasma arc welding 21 : Resistance spot welding 22 : Resistance seam welding 24 : Flash welding 42 : Friction welding 51 : Electron beam welding 52 : Laser welding 91 : Brazing with local heating 111 : Shielded metal arc welding 141 : Gas tungsten arc welding 522 : Gas laser welding 521 : Solid state laser welding 922 : Vacuum brazing 5) Published by: SAE, 400 Commonwealth Drive - Warrendale, PA 15096-0001 USA 6) Published by: AWS, 550 N.W LeJeune Road, Miami, Florida 33126 Copyright British Standards Institution Provided by IHS under license with BSI - Uncontrolled Copy No reproduction or networking permitted without license from IHS Not for Resale BS EN 4632-005:2009 EN 4632-005:2009 (E) Use of this standard The index of material sheets contained in this standard, classified by family based on the main element used in the chemical composition and on the alloy structure, is given in Clause The degree of weldability or brazeability (see EN 4632-001) to be used is the value indicated by the material sheet considered for the process chosen In the operating cycle, preferably select thermal states that give the lowest degree If two degrees are indicated, the responsible person shall select the degree that is most appropriate for the definition of the assembly Updating this standard See EN 4632-001 List of heat resisting Ni or Co base alloys Table `,,```,,,,````-`-`,,`,,`,`,,` - Sheet Material 7.1 NiCr15Fe 7.2 NiCr16Co10Mo8Al4Ti4 7.3 NiCr19Fe19Nb5Mo3 7.4 NiCr19Fe19Nb5Mo3 7.5 NiCr19Co11Mo10Ti3 7.6 NiCr20Co13Mo4Ti3Al 7.7 NiCr20Nb 7.8 NiCr20Ti 7.9 NiCr22Mo9Nb 7.10 NiCr22Mo9Nb 7.11 NiCr21Fe18Mo9 7.12 NiCr21Fe18Mo9 7.13 NiCr22Co13Mo9Al1 7.14 NiCo20Cr20Mo5Ti2Al 7.15 NiCo20Cr20Mo5Ti2Al 7.16 CoCr20W15Ni 7.17 CoCr26Ni11W 7.18 CoCr22Ni22W15 Copyright British Standards Institution Provided by IHS under license with BSI - Uncontrolled Copy No reproduction or networking permitted without license from IHS Not for Resale